View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 67181U 26145.55758524 +.00000000 +00000-0 +95971-3 0 00009
2 67181 43.0012 236.3829 0001601 277.8554 82.2116 15.27590400 07
| Epoch (UTC): | 25 May 2026 13:22:55 |
| Eccentricity: | 0.0001601 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.3829° |
| argument of perigee: | 277.8554° |
| revolutions per day: | 15.27590400 |
| mean anomaly at epoch: | 82.2116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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